A new one‐point quadrature enhanced assumed strain (EAS) solid‐shell element with multiple integration points along thickness: Part I—geometrically linear applications |
| |
Authors: | Ricardo J. Alves de Sousa,Rui P.R. Cardoso,Robertt A. Fontes Valente,Jeong‐Whan Yoon,Jos J. Gr cio,Renato M. Natal Jorge |
| |
Affiliation: | Ricardo J. Alves de Sousa,Rui P.R. Cardoso,Robertt A. Fontes Valente,Jeong‐Whan Yoon,José J. Grácio,Renato M. Natal Jorge |
| |
Abstract: | Accuracy and efficiency are the main features expected in finite element method. In the field of low‐order formulations, the treatment of locking phenomena is crucial to prevent poor results. For three‐dimensional analysis, the development of efficient and accurate eight‐node solid‐shell finite elements has been the principal goal of a number of recent published works. When modelling thin‐ and thick‐walled applications, the well‐known transverse shear and volumetric locking phenomena should be conveniently circumvented. In this work, the enhanced assumed strain method and a reduced in‐plane integration scheme are combined to produce a new eight‐node solid‐shell element, accommodating the use of any number of integration points along thickness direction. Furthermore, a physical stabilization procedure is employed in order to correct the element's rank deficiency. Several factors contribute to the high computational efficiency of the formulation, namely: (i) the use of only one internal variable per element for the enhanced part of the strain field; (ii) the reduced integration scheme; (iii) the prevention of using multiple elements' layers along thickness, which can be simply replaced by any number of integration points within a single element layer. Implementation guidelines and numerical results confirm the robustness and efficiency of the proposed approach when compared to conventional elements well‐established in the literature. Copyright © 2004 John Wiley & Sons, Ltd. |
| |
Keywords: | finite element method solid‐shell reduced integration enhanced assumed strain physical stabilization thin‐shell structure |
|
|